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限制器对高超声速体表面热流数值模拟的影响

杨建龙 刘猛

杨建龙, 刘猛. 限制器对高超声速体表面热流数值模拟的影响[J]. 北京航空航天大学学报, 2014, 40(3): 417-421. doi: 10.13700/j.bh.1001-5965.2013.0253
引用本文: 杨建龙, 刘猛. 限制器对高超声速体表面热流数值模拟的影响[J]. 北京航空航天大学学报, 2014, 40(3): 417-421. doi: 10.13700/j.bh.1001-5965.2013.0253
Yang Jianlong, Liu Meng. Influence of limiters on numerical simulation of heating distributions for hypersonic bodies[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 417-421. doi: 10.13700/j.bh.1001-5965.2013.0253(in Chinese)
Citation: Yang Jianlong, Liu Meng. Influence of limiters on numerical simulation of heating distributions for hypersonic bodies[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 417-421. doi: 10.13700/j.bh.1001-5965.2013.0253(in Chinese)

限制器对高超声速体表面热流数值模拟的影响

doi: 10.13700/j.bh.1001-5965.2013.0253
详细信息
  • 中图分类号: V221

Influence of limiters on numerical simulation of heating distributions for hypersonic bodies

  • 摘要: 采用Roe的FDS(Flux Difference Splitting)差分格式结合min mod,van Leer和Osher-C限制器,对高超声速体外部流场进行数值模拟.研究了限制器对高超声速体气动力/热数值模拟的区别,对比分析了3种限制器对三维模型表面热流数值模拟结果的影响.研究表明,限制器对数值模拟精度有重要影响,且对气动热数值模拟的影响大于对气动力的影响;对简单或较复杂的气动外形,采用Roe的FDS格式结合min mod限制器获得的表面热特性比它结合van Leer和Osher-C限制器时要好,可为热防护设计提供可靠结果.

     

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出版历程
  • 收稿日期:  2013-05-10
  • 网络出版日期:  2014-03-20

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